Three dimensional latching dynamics and loads induced during Apollo spacecraft docking, using linear stiffness or flexibility matrices for structural elasticity
A technique for analyzing latching dynamics and loads induced during spacecraft docking
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 8TH ; 1970 ; NEW YORK, NY
1970-01-01
Conference paper
No indication
English
Skylab experience with Apollo docking/latching loads
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